Date:
March 14th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9966 5 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3097)
---------------------------------------
Vector Time (GMT): 2009/072/23:43:44
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4124153
64 A = 6727601
73 meter
Y = 597580
28 meter E =
0011186
Z = 5272268
62 I = 51
93553
XDOT = -1736
284074 Wp = 109
14112
YDOT = -7490
017043 meter/sec RA = 73
95970 deg
ZDOT = -511
947260 TA = 345
68372
MA = 345
71539
Ha = 197
481 n
mi
Hp = 184
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13530687
80 X = -4156141
06
Y = 1960565
21 feet Y = 551283
20 meter
Z = 17297469
23 Z = 5252155
77
XDOT = -5696
470058 XDOT = -1649
913466
YDOT = -24573
546729 feet/sec YDOT = -7508
950306 meter/sec
ZDOT = -1679
616995 ZDOT = -520
171654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13720230
61 X = 4181926
29
Y = 1178085
12 feet Y = 359080
34 meter
Z = 17218976
68 Z = 5248344
09
XDOT = 57
860869 XDOT = 17
635993
YDOT = 24222
457599 feet/sec YDOT = 7383
005076 meter/sec
ZDOT = -1712
296149 ZDOT = -521
907866
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09073
03555741
00010596 00000-0 82463-4 0 9009
2 25544 51
6372 74
4110 0009303 120
7768 239
4311 15
71398305 30984
Satellite: ISS
Catalog Number: 25544
Epoch time: 09073
03555741 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 74
4110 deg
Eccentricity:
0009303
Arg of perigee: 120
7768 deg
Mean anomaly: 239
4311 deg
Mean motion: 15
71398305 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3098
Checksum: 293
Coasting Arc #2 (Orbit 3112)
---------------------------------------
Vector Time (GMT): 2009/073/23:43:44
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2716831
76 A = 6739377
36 meter
Y = 6152782
58 meter E =
0015645
Z = -403466
90 I = 51
96633
XDOT = -4201
689060 Wp = 78
24313
YDOT = 2238
431935 meter/sec RA = 68
86511 deg
ZDOT = 6041
884782 TA = 277
39688
MA = 277
57464
Ha = 197
240 n
mi
Hp = 184
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8913490
04 X = 2649788
37
Y = 20186294
54 feet Y = 6182788
88 meter
Z = -1323710
29 Z = -390431
79
XDOT = -13785
069093 XDOT = -4255
757675
YDOT = 7343
936793 feet/sec YDOT = 2191
144291 meter/sec
ZDOT = 19822
456634 ZDOT = 6021
341504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4488437
06 X = -1368075
62
Y = -21608425
22 feet Y = -6586248
01 meter
Z = -1272357
17 Z = -387814
46
XDOT = 13554
917166 XDOT = 4131
538752
YDOT = -3938
018810 feet/sec YDOT = -1200
308133 meter/sec
ZDOT = 19742
402253 ZDOT = 6017
484207
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09073
98945117
00010596 00000-0 82463-4 0 9014
2 25544 51
6372 69
5298 0009336 124
7470 235
4573 15
71447447 31132
Satellite: ISS
Catalog Number: 25544
Epoch time: 09073
98945117 = yrday
fracday
Element set: 901
Inclination: 51
6372 deg
RA of node: 69
5298 deg
Eccentricity:
0009336
Arg of perigee: 124
7470 deg
Mean anomaly: 235
4573 deg
Mean motion: 15
71447447 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3113
Checksum: 326
Coasting Arc #3 (Orbit 3128)
---------------------------------------
Vector Time (GMT): 2009/074/23:43:44
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2961651
02 A = 6727914
95 meter
Y = -3155091
59 meter E =
0021602
Z = -5169199
78 I = 51
91662
XDOT = 4268
238701 Wp = 98
69666
YDOT = 6238
078299 meter/sec RA = 63
78524 deg
ZDOT = -1370
077912 TA = 158
25261
MA = 158
16076
Ha = 197
222 n
mi
Hp = 184
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9716702
82 X = 3021822
68
Y = -10351350
35 feet Y = -3121636
48 meter
Z = -16959316
86 Z = -5154665
79
XDOT = 14003
407811 XDOT = 4204
821828
YDOT = 20466
136151 feet/sec YDOT = 6285
453585 meter/sec
ZDOT = -4495
006273 ZDOT = -1349
497155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11627033
57 X = -3543919
83
Y = 8263837
25 feet Y = 2518817
60 meter
Z = -16902789
14 Z = -5151970
13
XDOT = -9215
100166 XDOT = -2808
762531
YDOT = -21940
095280 feet/sec YDOT = -6687
341041 meter/sec
ZDOT = -4414
191014 ZDOT = -1345
445421
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09075
00692771
00010596 00000-0 82463-4 0 9025
2 25544 51
6377 64
3240 0009496 128
0779 232
1241 15
71473456 31295
Satellite: ISS
Catalog Number: 25544
Epoch time: 09075
00692771 = yrday
fracday
Element set: 902
Inclination: 51
6377 deg
RA of node: 64
3240 deg
Eccentricity:
0009496
Arg of perigee: 128
0779 deg
Mean anomaly: 232
1241 deg
Mean motion: 15
71473456 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3129
Checksum: 310
Coasting Arc #4 (Orbit 3144)
---------------------------------------
Vector Time (GMT): 2009/075/23:43:44
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4566884
39 A = 6737657
33 meter
Y = -4524562
02 meter E =
0023024
Z = 1975710
63 I = 51
93533
XDOT = 2261
760815 Wp = 119
97700
YDOT = -4755
540884 meter/sec RA = 58
65932 deg
ZDOT = -5625
331314 TA = 38
11454
MA = 37
95192
Ha = 197
078 n
mi
Hp = 184
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14983216
50 X = -4525548
18
Y = -14844363
58 feet Y = -4575400
40 meter
Z = 6481990
27 Z = 1953625
32
XDOT = 7420
475116 XDOT = 2342
096727
YDOT = -15602
168256 feet/sec YDOT = -4729
799542 meter/sec
ZDOT = -18455
811396 ZDOT = -5614
148439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12173450
36 X = 3710467
67
Y = 17256121
22 feet Y = 5259665
75 meter
Z = 6395427
36 Z = 1949326
26
XDOT = -8897
118761 XDOT = -2711
841798
YDOT = 13146
382580 feet/sec YDOT = 4007
017410 meter/sec
ZDOT = -18412
476286 ZDOT = -5612
122772
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09076
02439064
00010596 00000-0 82463-4 0 9033
2 25544 51
6376 59
1174 0009269 132
4310 227
7638 15
71500691 31450
Satellite: ISS
Catalog Number: 25544
Epoch time: 09076
02439064 = yrday
fracday
Element set: 903
Inclination: 51
6376 deg
RA of node: 59
1174 deg
Eccentricity:
0009269
Arg of perigee: 132
4310 deg
Mean anomaly: 227
7638 deg
Mean motion: 15
71500691 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3145
Checksum: 303
Coasting Arc #5 (Orbit 3160)
---------------------------------------
Vector Time (GMT): 2009/076/23:43:44
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -802361
44 A = 6730327
91 meter
Y = 4902924
12 meter E =
0017780
Z = 4533207
17 I = 51
89485
XDOT = -5886
832133 Wp = 125
26012
YDOT = -3863
899655 meter/sec RA = 53
60258 deg
ZDOT = 3118
489901 TA = 293
67559
MA = 293
86208
Ha = 197
013 n
mi
Hp = 184
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2632419
42 X = -879148
49
Y = 16085709
07 feet Y = 4893522
41 meter
Z = 14872726
92 Z = 4529122
70
XDOT = -19313
753718 XDOT = -5858
336811
YDOT = -12676
836137 feet/sec YDOT = -3929
570248 meter/sec
ZDOT = 10231
266079 ZDOT = 3089
961139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5241966
18 X = 1597751
29
Y = -15448805
20 feet Y = -4708795
82 meter
Z = 14857115
57 Z = 4528448
82
XDOT = 15983
398876 XDOT = 4871
739978
YDOT = 15214
089667 feet/sec YDOT = 4637
254531 meter/sec
ZDOT = 10119
588787 ZDOT = 3084
450662
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09077
04184309
00010596 00000-0 82463-4 0 9046
2 25544 51
6379 53
9114 0009430 136
6890 223
5014 15
71524243 31617
Satellite: ISS
Catalog Number: 25544
Epoch time: 09077
04184309 = yrday
fracday
Element set: 904
Inclination: 51
6379 deg
RA of node: 53
9114 deg
Eccentricity:
0009430
Arg of perigee: 136
6890 deg
Mean anomaly: 223
5014 deg
Mean motion: 15
71524243 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3161
Checksum: 293
Coasting Arc #6 (Orbit 3175)
---------------------------------------
Vector Time (GMT): 2009/077/23:43:44
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5429809
04 A = 6734343
14 meter
Y = 2116707
05 meter E =
0013170
Z = -3391476
99 I = 51
89093
XDOT = 525
642454 Wp = 122
80557
YDOT = 6093
751684 meter/sec RA = 48
45591 deg
ZDOT = 4650
871590 TA = 197
45931
MA = 197
50463
Ha = 197
003 n
mi
Hp = 185
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17814334
13 X = 5422211
15
Y = 6944576
94 feet Y = 2177383
78 meter
Z = -11126893
00 Z = -3365117
71
XDOT = 1724
548735 XDOT = 434
869147
YDOT = 19992
623634 feet/sec YDOT = 6099
122285 meter/sec
ZDOT = 15258
765058 ZDOT = 4653
204518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16710778
37 X = -5093445
25
Y = -9413338
92 feet Y = -2869185
70 meter
Z = -11023807
60 Z = -3360056
56
XDOT = 533
406619 XDOT = 162
582338
YDOT = -18803
923903 feet/sec YDOT = -5731
436006 meter/sec
ZDOT = 15268
292114 ZDOT = 4653
775436
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09077
99569427
00010596 00000-0 82463-4 0 9059
2 25544 51
6391 49
0310 0009600 139
6141 220
5736 15
71524718 31767
Satellite: ISS
Catalog Number: 25544
Epoch time: 09077
99569427 = yrday
fracday
Element set: 905
Inclination: 51
6391 deg
RA of node: 49
0310 deg
Eccentricity:
0009600
Arg of perigee: 139
6141 deg
Mean anomaly: 220
5736 deg
Mean motion: 15
71524718 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3176
Checksum: 316
Coasting Arc #7 (Orbit 3191)
---------------------------------------
Vector Time (GMT): 2009/078/23:43:44
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1742635
69 A = 6733727
56 meter
Y = -5463968
86 meter E =
0012993
Z = -3531361
29 I = 51
86886
XDOT = 6155
424557 Wp = 122
37140
YDOT = 943
129931 meter/sec RA = 43
40681 deg
ZDOT = -4515
628165 TA = 99
43094
MA = 99
28404
Ha = 196
863 n
mi
Hp = 185
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5717308
70 X = -1664252
65
Y = -17926407
01 feet Y = -5483017
87 meter
Z = -11585830
99 Z = -3539636
36
XDOT = 20194
962457 XDOT = 6166
356690
YDOT = 3094
258305 feet/sec YDOT = 1012
024467 meter/sec
ZDOT = -14815
053036 ZDOT = -4485
698934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3365445
69 X = 1025787
85
Y = 18492132
46 feet Y = 5636401
97 meter
Z = -11618518
81 Z = -3541324
53
XDOT = -18386
062930 XDOT = -5604
071981
YDOT = -5849
945422 feet/sec YDOT = -1783
063365 meter/sec
ZDOT = -14698
103678 ZDOT = -4479
982001
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09079
01312213
00010596 00000-0 82463-4 0 9064
2 25544 51
6393 43
8248 0009507 143
2837 216
8978 15
71546541 31922
Satellite: ISS
Catalog Number: 25544
Epoch time: 09079
01312213 = yrday
fracday
Element set: 906
Inclination: 51
6393 deg
RA of node: 43
8248 deg
Eccentricity:
0009507
Arg of perigee: 143
2837 deg
Mean anomaly: 216
8978 deg
Mean motion: 15
71546541 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3192
Checksum: 316
Coasting Arc #8 (Orbit 3207)
---------------------------------------
Vector Time (GMT): 2009/079/23:43:44
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5032418
24 A = 6730780
34 meter
Y = 466367
75 meter E =
0014718
Z = 4430751
05 I = 51
83610
XDOT = -3469
112050 Wp = 108
67738
YDOT = -6038
432140 meter/sec RA = 38
25552 deg
ZDOT = -3300
350088 TA = 14
34665
MA = 14
30490
Ha = 196
996 n
mi
Hp = 185
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16510558
54 X = -5058782
73
Y = 1530077
93 feet Y = 409945
09 meter
Z = 14536584
82 Z = 4406239
84
XDOT = -11381
601214 XDOT = -3385
299172
YDOT = -19811
129067 feet/sec YDOT = -6076
757288 meter/sec
ZDOT = -10827
920235 ZDOT = -3316
998975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16662539
77 X = 5078742
12
Y = 269204
47 feet Y = 82053
52 meter
Z = 14440889
08 Z = 4401582
99
XDOT = 9134
794835 XDOT = 2784
285466
YDOT = 19701
789910 feet/sec YDOT = 6005
105565 meter/sec
ZDOT = -10893
349454 ZDOT = -3320
292914
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09080
03053873
00010596 00000-0 82463-4 0 9073
2 25544 51
6391 38
6184 0009623 147
2895 212
8863 15
71531814 32082
Satellite: ISS
Catalog Number: 25544
Epoch time: 09080
03053873 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 38
6184 deg
Eccentricity:
0009623
Arg of perigee: 147
2895 deg
Mean anomaly: 212
8863 deg
Mean motion: 15
71531814 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3208
Checksum: 315
Coasting Arc #9 (Orbit 3223)
---------------------------------------
Vector Time (GMT): 2009/080/23:43:44
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4201717
83 A = 6736889
90 meter
Y = 4792083
03 meter E =
0018288
Z = 2175281
60 I = 51
83500
XDOT = -5027
535335 Wp = 102
06474
YDOT = 1887
018263 meter/sec RA = 33
19543 deg
ZDOT = 5511
443997 TA = 282
19290
MA = 282
39768
Ha = 196
641 n
mi
Hp = 185
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13785163
48 X = 4137252
70
Y = 15722057
20 feet Y = 4838708
77 meter
Z = 7136750
66 Z = 2195536
39
XDOT = -16494
538502 XDOT = -5075
035855
YDOT = 6191
004801 feet/sec YDOT = 1830
532165 meter/sec
ZDOT = 18082
165345 ZDOT = 5486
905091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12259668
46 X = -3736746
95
Y = -16904860
96 feet Y = -5152601
62 meter
Z = 7216178
35 Z = 2199491
16
XDOT = 15859
567996 XDOT = 4833
996325
YDOT = -3764
768556 feet/sec YDOT = -1147
501456 meter/sec
ZDOT = 17986
457304 ZDOT = 5482
272186
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09081
04793950
00010596 00000-0 82463-4 0 9083
2 25544 51
6405 33
4125 0009618 151
7670 208
4016 15
71611711 32245
Satellite: ISS
Catalog Number: 25544
Epoch time: 09081
04793950 = yrday
fracday
Element set: 908
Inclination: 51
6405 deg
RA of node: 33
4125 deg
Eccentricity:
0009618
Arg of perigee: 151
7670 deg
Mean anomaly: 208
4016 deg
Mean motion: 15
71611711 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3224
Checksum: 288
Coasting Arc #10 (Orbit 3238)
---------------------------------------
Vector Time (GMT): 2009/081/23:43:44
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3527229
14 A = 6727877
89 meter
Y = -2662646
84 meter E =
0020791
Z = -5090473
18 I = 51
77932
XDOT = 5901
479238 Wp = 123
55953
YDOT = 4628
461445 meter/sec RA = 28
05761 deg
ZDOT = 1661
809793 TA = 162
45958
MA = 162
38767
Ha = 196
557 n
mi
Hp = 185
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11572274
08 X = 3581469
42
Y = -8735717
97 feet Y = -2622900
42 meter
Z = -16701027
51 Z = -5073206
18
XDOT = 19361
808524 XDOT = 5841
211734
YDOT = 15185
240962 feet/sec YDOT = 4694
118380 meter/sec
ZDOT = 5452
131868 ZDOT = 1690
332051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12280228
79 X = -3743013
74
Y = 7852909
13 feet Y = 2393566
70 meter
Z = -16633773
31 Z = -5069974
10
XDOT = -17586
651232 XDOT = -5360
411296
YDOT = -15671
969938 feet/sec YDOT = -4776
816437 meter/sec
ZDOT = 5563
835397 ZDOT = 1695
857029
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09082
00174432
00010596 00000-0 82463-4 0 9099
2 25544 51
6407 28
5325 0009521 154
7395 205
4234 15
71613361 32392
Satellite: ISS
Catalog Number: 25544
Epoch time: 09082
00174432 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 28
5325 deg
Eccentricity:
0009521
Arg of perigee: 154
7395 deg
Mean anomaly: 205
4234 deg
Mean motion: 15
71613361 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3239
Checksum: 291
Coasting Arc #11 (Orbit 3254)
---------------------------------------
Vector Time (GMT): 2009/082/23:43:44
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5921560
47 A = 6738709
32 meter
Y = -3115261
34 meter E =
0019746
Z = -707966
10 I = 51
78970
XDOT = 2783
922346 Wp = 148
62273
YDOT = -3949
121123 meter/sec RA = 22
97040 deg
ZDOT = -5998
909742 TA = 39
07300
MA = 38
93055
Ha = 196
392 n
mi
Hp = 185
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19427691
82 X = -5882845
86
Y = -10220673
67 feet Y = -3181263
28 meter
Z = -2322723
41 Z = -736638
39
XDOT = 9133
603499 XDOT = 2857
016479
YDOT = -12956
434132 feet/sec YDOT = -3917
581553 meter/sec
ZDOT = -19681
462407 ZDOT = -5985
207680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18805785
09 X = 5732003
30
Y = 11300712
26 feet Y = 3444457
10 meter
Z = -2434907
31 Z = -742159
75
XDOT = -9140
086193 XDOT = -2785
898272
YDOT = 11042
387660 feet/sec YDOT = 3365
719759 meter/sec
ZDOT = -19628
219746 ZDOT = -5982
681378
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09083
01912236
00010596 00000-0 82463-4 0 9105
2 25544 51
6411 23
3253 0009465 158
7725 201
3832 15
71624725 32551
Satellite: ISS
Catalog Number: 25544
Epoch time: 09083
01912236 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 23
3253 deg
Eccentricity:
0009465
Arg of perigee: 158
7725 deg
Mean anomaly: 201
3832 deg
Mean motion: 15
71624725 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3255
Checksum: 286
Coasting Arc #12 (Orbit 3270)
---------------------------------------
Vector Time (GMT): 2009/083/23:43:44
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1176616
27 A = 6726749
81 meter
Y = 3996032
49 meter E =
0010392
Z = 5277359
18 I = 51
72328
XDOT = -7351
528555 Wp = 149
90504
YDOT = -2294
194959 meter/sec RA = 17
85534 deg
ZDOT = 89
210961 TA = 299
19756
MA = 299
30148
Ha = 196
243 n
mi
Hp = 185
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3860289
59 X = -1246849
41
Y = 13110342
82 feet Y = 3982482
75 meter
Z = 17314170
53 Z = 5271472
19
XDOT = -24119
188174 XDOT = -7325
761470
YDOT = -7526
886347 feet/sec YDOT = -2376
259957 meter/sec
ZDOT = 292
686880 ZDOT = 53
560309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4472358
01 X = 1363174
72
Y = -12944772
18 feet Y = -3945566
56 meter
Z = 17291452
01 Z = 5270434
57
XDOT = 22862
182824 XDOT = 6968
393325
YDOT = 8142
611076 feet/sec YDOT = 2481
867856 meter/sec
ZDOT = 153
312752 ZDOT = 46
729727
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09084
03648698
00010596 00000-0 82463-4 0 9117
2 25544 51
6422 18
1195 0009345 162
9284 197
2194 15
71666479 32718
Satellite: ISS
Catalog Number: 25544
Epoch time: 09084
03648698 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 18
1195 deg
Eccentricity:
0009345
Arg of perigee: 162
9284 deg
Mean anomaly: 197
2194 deg
Mean motion: 15
71666479 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3271
Checksum: 335
Coasting Arc #13 (Orbit 3285)
---------------------------------------
Vector Time (GMT): 2009/084/23:43:44
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6636972
43 A = 6738587
23 meter
Y = 818541
28 meter E =
0008885
Z = -842805
33 I = 51
73492
XDOT = 151
542079 Wp = 96
09719
YDOT = 4854
672323 meter/sec RA = 12
73596 deg
ZDOT = 5961
004621 TA = 254
73895
MA = 254
83720
Ha = 196
165 n
mi
Hp = 185
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21774843
92 X = 6631420
28
Y = 2685502
89 feet Y = 892728
64 meter
Z = -2765109
35 Z = -810576
54
XDOT = 497
185300 XDOT = 68
287609
YDOT = 15927
402633 feet/sec YDOT = 4855
902113 meter/sec
ZDOT = 19557
101776 ZDOT = 5961
538050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21725809
87 X = -6622026
85
Y = -3166285
81 feet Y = -965083
91 meter
Z = -2639204
95 Z = -804429
67
XDOT = -262
991652 XDOT = -80
159855
YDOT = -14347
898607 feet/sec YDOT = -4373
239495 meter/sec
ZDOT = 19559
512174 ZDOT = 5961
739311
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09084
99025610
00010596 00000-0 82463-4 0 9126
2 25544 51
6427 13
2391 0009310 165
9595 194
1828 15
71647924 32867
Satellite: ISS
Catalog Number: 25544
Epoch time: 09084
99025610 = yrday
fracday
Element set: 912
Inclination: 51
6427 deg
RA of node: 13
2391 deg
Eccentricity:
0009310
Arg of perigee: 165
9595 deg
Mean anomaly: 194
1828 deg
Mean motion: 15
71647924 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3286
Checksum: 323
Coasting Arc #14 (Orbit 3301)
---------------------------------------
Vector Time (GMT): 2009/085/23:43:44
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1434604
22 A = 6727758
68 meter
Y = -4220791
54 meter E =
0015881
Z = -5049798
06 I = 51
66987
XDOT = 7466
787822 Wp = 112
38216
YDOT = -418
823382 meter/sec RA = 7
64552 deg
ZDOT = -1781
556486 TA = 140
49339
MA = 140
37752
Ha = 196
007 n
mi
Hp = 185
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4706706
77 X = -1362768
89
Y = -13847741
26 feet Y = -4236432
99 meter
Z = -16567578
92 Z = -5056592
46
XDOT = 24497
335373 XDOT = 7479
570742
YDOT = -1374
092462 feet/sec YDOT = -335
254119 meter/sec
ZDOT = -5845
001595 ZDOT = -1745
251588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4543014
50 X = 1384710
82
Y = 13870288
49 feet Y = 4227663
93 meter
Z = -16594391
05 Z = -5057970
39
XDOT = -23525
710923 XDOT = -7170
636689
YDOT = 922
774849 feet/sec YDOT = 281
261774 meter/sec
ZDOT = -5703
271668 ZDOT = -1738
357204
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09086
00759657
00010596 00000-0 82463-4 0 9136
2 25544 51
6430 8
0332 0009325 170
6732 189
4605 15
71664534 33025
Satellite: ISS
Catalog Number: 25544
Epoch time: 09086
00759657 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 8
0332 deg
Eccentricity:
0009325
Arg of perigee: 170
6732 deg
Mean anomaly: 189
4605 deg
Mean motion: 15
71664534 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3302
Checksum: 301
Coasting Arc #15 (Orbit 3317)
---------------------------------------
Vector Time (GMT): 2009/086/23:43:44
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6150684
96 A = 6736659
31 meter
Y = 1516237
41 meter E =
0019904
Z = 2254879
40 I = 51
66998
XDOT = -3108
116151 Wp = 133
38250
YDOT = -4458
867792 meter/sec RA = 2
49653 deg
ZDOT = -5463
231842 TA = 21
30957
MA = 21
22679
Ha = 195
997 n
mi
Hp = 186
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20179412
60 X = -6178136
54
Y = 4974532
20 feet Y = 1447303
58 meter
Z = 7397898
30 Z = 2224932
30
XDOT = -10197
231468 XDOT = -3031
485712
YDOT = -14628
831339 feet/sec YDOT = -4493
196573 meter/sec
ZDOT = -17923
988982 ZDOT = -5478
144676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20159088
42 X = 6144490
15
Y = -5223094
94 feet Y = -1591999
34 meter
Z = 7281071
09 Z = 2219270
47
XDOT = 9891
844263 XDOT = 3015
034131
YDOT = 13033
637981 feet/sec YDOT = 3972
652857 meter/sec
ZDOT = -17982
509985 ZDOT = -5481
069043
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09087
02492511
00010596 00000-0 82463-4 0 9143
2 25544 51
6427 2
8277 0009393 173
5439 186
5845 15
71678042 33182
Satellite: ISS
Catalog Number: 25544
Epoch time: 09087
02492511 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 2
8277 deg
Eccentricity:
0009393
Arg of perigee: 173
5439 deg
Mean anomaly: 186
5845 deg
Mean motion: 15
71678042 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3318
Checksum: 325
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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